DocumentCode
359065
Title
Non-fragile H∞ flight controller design for a high performance aircraft
Author
Yee, Jiong-Sang ; Yang, Guang-Hong ; Wang, Jian Liang
Author_Institution
Sch. of Electr. & Electron. Eng., Nanyang Technol. Univ., Singapore
Volume
3
fYear
2000
fDate
2000
Firstpage
1857
Abstract
Studies the design of non-fragile H∞ output-feedback control for a high performance aircraft in executing a large bank-angle maneuver. The designed flight controller tolerates some multiplicative gain variations in the controller matrices. Through linear and nonlinear simulation results, the paper demonstrates the advantage of designing the non-fragile H∞ flight controller for practical implementation
Keywords
H∞ control; aircraft control; control system synthesis; feedback; matrix algebra; robust control; uncertain systems; high performance aircraft; large bank-angle maneuver; linear simulation; multiplicative gain variations; nonfragile H∞ flight controller; nonlinear simulation; Actuators; Aerospace control; Aircraft; Automatic control; Control systems; Degradation; Digital control; Error correction; Quantization; Roundoff errors;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2000. Proceedings of the 2000
Conference_Location
Chicago, IL
ISSN
0743-1619
Print_ISBN
0-7803-5519-9
Type
conf
DOI
10.1109/ACC.2000.879523
Filename
879523
Link To Document